BRAND and MODEL
BELL 214ST
TYPE
General purpose utility helicopter
ORIGIN
United States of America
ENGINE
Two 1,212 kw (1,625 shp) General Electric CT7-2A turboshafts limited to a combined output of 1,678
kw (2,250 shp)
SPECIFICATIONS
Rotor diameter: 15.85 m (52 ft)
Overall length: 18.95 m (62 ft 2 in)
Fuselage length: 15.03 m (49 ft 4 in)
Height: 4.85 m (15 ft 11 in)
Main rotor disc area: 197.4 m² (2,124 sq ft)
Max cruising speed at 1,219 m (4,000 ft): 260 km/h (162 mph)
Max cruising speed at sea level: 264 km/h (164 mph)
Economical cruising speed: 249 km/h (155 mph)
Max initial rate of climb: 543 m/min (1,780 ft/min)
Hovering ceiling out of ground effect: 1,830 m (6,000 ft)
Single-engine ceiling: 2,440 m (8,000 ft)
Range with 20 mins reserve: 740 km (460 miles)
Empty weight: 4,300 kg (9,481 lb)
Loaded weight: 7,938 kg (17,500 lb)
PHOTO
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